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NOVOTECH AEROSPACE ADVANCED TECHNOLOGY SRL
Acronimo
NOVOTECH
Partita Iva
03256501218
Codice ATECO
62.01.00
PRODUZIONE DI SOFTWARE, CONSULENZA INFORMATICA E ATTIVITÀ CONNESSE
Data di costituzione
26/03/2013
Descrizione sintetica dell'oggetto sociale
NOVOTECH is a key partner for many industries working in the aerospace field and other advanced technology sectors. NOVOTECH has developed well consolidated know-how on aircraft and aircraft components: design/certification; automated composite manufacturing processes; advanced FEA; static/dynamic experimental tests.NOVOTECH has proven capability in design and manufacturing of composite structures, based on low cost and out-of-autoclave automated production processes (as AFP, PCM, RTM and LRI). The Company can count on researchers and qualified engineers for the development and manufacturing of composite prototypes with complex shapes and variable thickness based on advanced design methodologies for draping and formability and composite warpage prediction.
'This is a proposal for a research project that aims to fulfill the objectives as set up in the Call SP1-JTI-CS-2013-01-GRA-02-023. Therefore is will investigate advanced design and simulation methods for Load control and alleviation devices and high lift devices. The research will focus on novel methods for modelling of aerodynamic loads on flexible bodies, modelling of actuators and methods for coupled simulation. The novel methods will be evaluated in context of preliminary and detailed design studies of 4 mechanisms as specified in the call: 1. Krueger Flap (GTF) 2. Single Slotted Flap (GTF) 3. LC&A devices 4. Single Slotted Flap (TP) NOVOTECH will be responsible for the preliminary design studies and knowledge transfer. LMS will be responsible for the detailed conceptual designs and management of the project.'
NHYTE project aims at developing and demonstrating concepts and methodologies enabling the realization of innovative integrated aero-structures, made of a new hybrid thermoplastic matrix composite material with multifunctional capabilities. The high-performing material proposed, based on a commercial PEEK-Carbon Fiber Prepreg with addition of amorphous (PEI) films, answers to the needs to have reduced weight and consequently reduced fuel consumptions and emissions on an aircraft, as well as reduced manufacturing and operational costs. Demonstration aero-structures will be fabricated by an innovative working cell implementing an advanced continuous automated production process, including: automated hybrid material fabrication; manufacturing of skin panels by automated fiber placement in-situ consolidation process; fabrication of stringers by continuous forming; component assembly by induction welding. The innovative material, conceived and patented by a partner of the Consortium, is an example of multifunctional composite, since it returns both functions of toughness improvement (multilayer material) and process simplification. This concept on one side will provide an advantage from the structural point of view, in terms of better impact damage performance; while on the other side major advantages will result on processing simplification, in particular including improved cycle times and lower energy consumptions, since it does not require the use of an autoclave curing phase. As of today, its usage has been limited to fabricate panels, only at laboratory level; hence, a suitable improvement finalized to process in industrial environment is needed. Proposed process techniques and assembly will be the first step towards the industrial application of the innovative material. Consortium has set a target for weight saving not less than 5% for primary structures. Further reduction of full life cycle cost is expected from scrape material and end of life structures recycling.
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